Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms PDF Download

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Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms

Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms PDF Author: Harvard Lomax
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 48

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Book Description
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.